# Service difficulty reports: N747DH, cancelled Oct 31, 2017

A list on [N747DH, cancelled Oct 31, 2017](https://openairdocs.org/deregistered/N747DH-2017-10-31.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 124 reports

- [SDR DHLA200800036](https://openairdocs.org/sdr/DHLA200800036.md): Wire · damaged · Mar 25, 2008 · N747DH · Boeing 727224 · Ice/Rain Protection System Wiring
  > ON GROUND BURNING ELECTRICAL SMELL IN COCKPIT AFT OF CAPTS SEAT (L-2 WINDOW WIRING) L-2 HEAT INOP. TRANSFERRED TO DEFER LOG NR 32178 IAW MEL 30-15-1 CAT C PLACARD INSTALLED DMI. REPAIRED WIRING AS PER SWPM 20-10-13 AND 727-200 WIRING DIAG 30-41-12 PG 5. SY
- [SDR 2008747001](https://openairdocs.org/sdr/2008747001.md): Wedge · delaminated · Mar 21, 2008 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > UPON INSPECTION TO THE EXTERIOR OF THE AIRCRAFT, FOUND THE LEFT INBOARD TRAILING EDGE MIDFLAP WEDGE DELAMINATED AT WBL 203.0 4 1/2 BY 2 1/2 AREA OF DELAMINATION. REPAIRED BY FLIGHTSTAR AIRCRAFT SERVICES USING BOEING SRM 51-40-20,51-50--2 AND 51-40-21. THIS I
- [SDR DHL2007747001](https://openairdocs.org/sdr/DHL2007747001.md): Skin · gouged · Jan 5, 2007 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > RT INBD FORE FLAP O/B LEADING EDGE HAS GOUGE ON REPAIR DOUBLER. REMOVED AND REPLACED DAMAGED REPAIR FROM RT INBD FORE FLAP O/B LEADING EDGE IAW B727 SRM 57-50-4.
- [SDR DHL2006747003](https://openairdocs.org/sdr/DHL2006747003.md): Battery · no test · Sep 19, 2006 · N747DH · Boeing 727224 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED LIGHT ASSY. BATTERIES, OPS CK. NORMAL IAW BMM REF 33-50-01. P/N 37067-001.
- [SDR DHL2006747002](https://openairdocs.org/sdr/DHL2006747002.md): Fairing · damaged · Mar 13, 2006 · N747DH · Boeing 727224 · Aerodynamic Fairings
  > MX RELEASE FOR DROP IN VISIT FOR DAMAGE TO LT AFT BODY FAIRING AND FAIRING SUPPORT. MX RELEASE DONE ON 3-13-06 UNDER WORK ORDER 5001328.
- [SDR DHL2006747001](https://openairdocs.org/sdr/DHL2006747001.md): Pin · installed · Mar 1, 2006 · N747DH · Boeing 727224 · Main Landing Gear
  > NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD NOSE GEAR PIN FOUND INSTALLED ON POST FLIGHT. DURING POST FLT FOUND ONE MAIN GEAR PIN MISSING. REMOVED NOSE GEAR PIN AND STOWED IAW ASTAR GMM 20.7. VERIFIED MAIN GEAR PINS REMOVED FROM GEAR. ENTERED MISSING G
- [SDR DHL2005747003](https://openairdocs.org/sdr/DHL2005747003.md): Connector · loose · Dec 16, 2005 · N747DH · Boeing 727224 · Leading Edge Slat Control System
  > AFTER FLAPS WERE RETRACTED TO 0 THE AMBER LE FLAPS LIGHT ILLUMINATED ON FWD PANEL SO PANEL READ NR5 LE FLAP IN TRANSIT ABNORMAL PROCEDURE COMPLETE PROBLEM REMAINED. FOUND CONNECTOR LOOSE FOR SWITCH CLEANED, RESECURED SWITCH CONNECTOR PLUG RAN FLAPS OPS CK NML
- [SDR DHL2005747001](https://openairdocs.org/sdr/DHL2005747001.md): Wire · chafed · Nov 8, 2005 · N747DH · Boeing 727224 · Electrical Power System Wiring
  > NR 1 GEN FAILED ON T/O ROLL DISCONECTED CSD RTO INFO OAT 16 C PA 4300 SPEED 45 KNOTS MODERATE BREAKING A/C WEIGHT 131,400 REV. THRUST MODERATE. DEFERRED IAW MEL 24-1CAT B CONTROL NR 23128 MC INATALS KPS. TRANSFERED TO DMI GREEN SHEET. C/W SPECIAL PROCEDUR
- [SDR DHL2005747002](https://openairdocs.org/sdr/DHL2005747002.md): Smoke · detected · Nov 8, 2005 · N747DH · Boeing 727224 · Air Distribution System
  > COCKPIT FILLED WITH SMOKE, EVACUATED A/C. WITH ENGINE PNEUMATICS RAN BOTH A/C PACKS AND INSPECTED FOR SMOKE SOURCE, NO DEFECTS A/C OK FOR SERVICE IAW MM JRH 6.3.
- [SDR DHL2005747511](https://openairdocs.org/sdr/DHL2005747511.md): Bear Strap · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AFT PIT INTERNAL SKIN STA 990 STR 28R AFT OF BEAR STRAP DOUBLER. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER 20.25 X 15.5 INCH FROM 2024-T3.160 IAW B737 SRM 53-30-3 FIG 3.
- [SDR DHL2005747510](https://openairdocs.org/sdr/DHL2005747510.md): Stringer · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR 28R, STA 950F TO 970 AT SKIN ATTACHMENTS. REMOVED STR 28R FROM 950F TO 1010, FRAME STA 987 RT CLIPS AND ANGLE SUPPORT STA 950F, 985, 990. FABRICATED AND INSTALLED STR SPLICE 13.5 INCH FROM BAC1498-131, SPLICE 1.08 X.810 X.19R FROM 70
- [SDR DHL2005747509](https://openairdocs.org/sdr/DHL2005747509.md): Shear Web · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Miscellaneous Structure
  > CORRODED AFT CARGO INTERCOSTAL FROM STA 950F TO 970 STR 28R. REMOVED FLOOR SUPPORT CLIPS, REMOVED SHEAR WEB. FABRICATED AND INSTALLED NEW SHEAR WEB 19.5 X 7 INCHES FROM 7075-T6.040 WEB, FLOOR SUPPORT CLIPS IAW B727 SRM 51-30-5, 51-10-2, 53-10-2 AND 51-30-2.
- [SDR DHL2005747508](https://openairdocs.org/sdr/DHL2005747508.md): Stringer Splice · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Main, Longeron/Stringer
  > CORRODED STRINGER SPLICE 28R IN AFT CARGO COMPT BS 1010. REMOVED CORRODED SPLICE. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE 12.5 INCHES FROM BAC1498-131 IAW B727 SRM 51-30-2 AND DWG 65-16341.
- [SDR DHL2005747507](https://openairdocs.org/sdr/DHL2005747507.md): Attach Angle · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Main, Attach Fittings
  > CORROSION ON SKIN ATTACH ANGLE FS 990 FROM STR 27R TO STR 29R. REMOVED CORROSION OFF SKIN ATTACH ANGLE FS 990 STR 27R TO 29R. PERFORMED ULT INSP ON BLENDED AREA. ATTACH ANGLE BEYOND LIMITS IAW B727 SRM 51-20-1. FABRICATED AND INSTALLED NEW ATTACH ANGLE SKI
- [SDR DHL2005747506](https://openairdocs.org/sdr/DHL2005747506.md): Shear Tie · corroded · Aug 14, 2005 · N747DH · Boeing 727224 · Fuselage Internal Mounting Structure
  > CORROSION ON AFT PIT FRAME AT BS 970 STR 28R - 29R. REMOVED FLOOR SUPPORT AND VERTICAL STIFFENER BS 930 - 990. ANGLE SHEAR TIE FOUND 100 PERCENT MATERIAL LOSS. CUT OUT CORRODED AREA OF ANGLE SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE REPAIR 6 X 1 X 1 IN
- [SDR DHL2005747502](https://openairdocs.org/sdr/DHL2005747502.md): Wedge · delaminated · Jul 27, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > LEFT WING INBD MID FLAP T/E WEDGE APPROX 61" FROM INBD END HAS AREA OF DELAMINATION ON BOTTOM SKIN. REPAIRED LEFT INBD MID FLAP T/E INNER BOTTOM SKIN AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.
- [SDR DHL2005747513](https://openairdocs.org/sdr/DHL2005747513.md): Web · corroded · Jul 17, 2005 · N747DH · Boeing 727224 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT STR 27L STA 950 TO STA 950A. REMOVED CORROSION ON WEB AT STA. 950 TO 950A LONGERON 27L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 AND 51-10-6. REMOVED WEB AND INSTALLED NEW WEB P/N 69-44877-13, ALODINED AND PRIMED IAW B727 SRM 51-10-2, INST
- [SDR DHL2005747512](https://openairdocs.org/sdr/DHL2005747512.md): Skin · gouged · Jul 17, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > LT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD LOWER LEADING EDGE REPAIR DOUBLER IS GOUGED THRU. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER 3.95 X 4.55 INCH FROM 2024-T3.063 IAW B727 SRM 57-50-4. ALODINED AND PRIMED, INST
- [SDR DHL2005747503](https://openairdocs.org/sdr/DHL2005747503.md): Skin · delaminated · Jul 12, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > LT WING INBD MID-FLAP T/E APPROX 61" FROM INBD END HAVE DELAMINATION. REPAIRED LT INBD MID FLAP T/E AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR.
- [SDR DHL2005747500](https://openairdocs.org/sdr/DHL2005747500.md): Web · corroded · Jul 12, 2005 · N747DH · Boeing 727224 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AFT CARGO BIN FS 950 TO FS 950A AT STR 27R. REMOVED CORROSION ON WEB IN AFT CARGO BIN FS 950 TO 950A AT STR 27R. FOUND OUT OF LIMITS. OPEN PANEL NR 3622 FOR ACCESS. REMOVED FLOOR SUPPORT SPLICE ANGLE SAT 950A TO 950B LONGERON 27R. REMOVED
- [SDR DHL2005747505](https://openairdocs.org/sdr/DHL2005747505.md): Skin · debonded · Jul 10, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > RT WING INBD MID FLAP T/E APPROX 1/2" FROM INBD END IS DISBONDED. CUT OUT DELAM AREA, FAB FILLER AN DOUBLERS ON TRAVELER NR T-828368. CLEANED UP AN PREP REPAIR AREA AN PARTS FAB. BONDED REPAIR PARTS, TREATED AND PRIMED. COMPLETED REPAIR ON RT WING I/B MID
- [SDR DHL2005747504](https://openairdocs.org/sdr/DHL2005747504.md): Skin · cracked · Jul 10, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > CRACK IN T/E FLAP LWR SKIN AT NR 3 ATTACH CUT OUT I/B SIDE LT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 57-50-4,51-10-2 AN 51-20-0 PG 1 OF MM AT T/E FLAP LOWER SKIN NR 3 ATTACH CUTOUT I/B SIDE OF LT WIN
- [SDR DHL2005747501](https://openairdocs.org/sdr/DHL2005747501.md): Skin · cracked · Jul 10, 2005 · N747DH · Boeing 727224 · Trailing Edge Flaps
  > CRACK IN T/E FLAP SHIM AT NR 2 ATTACH CUT OUT I/B SIDE LOWER SIDE LEFT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AN PRIMED AN INSTALLED REPAIR DOUBLER IAW B-727 SRM 57-50-4,51-10-2 AND 51-20-0 PG 1 OF B727 MM, AT T/E FLAP SKIN AT NR 2 ATTACH CUT OUT I/B L
- [SDR DHL2004747011](https://openairdocs.org/sdr/DHL2004747011.md): Switch · dirty · Dec 18, 2004 · N747DH · Boeing 727224 · Door Warning System
  > LEFT MAIN GEAR DOOR LIGHT ILLUM DURING TAKEOFF ROLL EXTINGUISHED DURING CLIMBOUT (RED LIGHT ON F/O PANEL). FOUND LEFT MAIN GEAR DOOR SWITCH CONTAMINATED. CLEANED SWITCH, CYCLED SEVERAL TIMES, FOUND TO BE MOVING FREELY. OPS CHECKS GOOD ON GROUND IAW MM 32-62
- [SDR DHL2004747010](https://openairdocs.org/sdr/DHL2004747010.md): Warning Light · illuminated · Dec 1, 2004 · N747DH · Boeing 727224 · Landing Gear Position and Warning
  > AFTER T/O FROM IAH, GEAR HANDLE PLACED TO OFF THE RED DOORS LIGHT AND RT DOOR LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES LIGHTS WENT OUT. WHEN GEAR HANDLE PLACED TO UP APPROACHING CVG PLACED GEAR HANDLE TEE. CYCLED RIGHT HAND GEAR DOOR SEVERAL TIME
- [SDR DHL2004747009](https://openairdocs.org/sdr/DHL2004747009.md): Actuator · inoperative · Nov 30, 2004 · N747DH · Boeing 727224 · Leading Edge Slat Actuator
  > "A" SYSTEM FAILED DURING LDG GEAR EXTENSION. PERFORMED ABNORMAL PROCEDURE AND LANDED. A/C TOWED IN. REMOVED AND REPLACED NR 1 SLAT ACTUATOR IAW M/M 27-81-31, NO LEAKS NOTED.
- [SDR DHL2004747008](https://openairdocs.org/sdr/DHL2004747008.md): Light · dislodged · Nov 10, 2004 · N747DH · Boeing 727224 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FELL OFF MOUNT DURING FLIGHT. SECURED LIGHT ASSEMBLY, OPS CHECK GOOD IAW 727 MM CH 33-50.
- [SDR DHL2004747007](https://openairdocs.org/sdr/DHL2004747007.md): Control Lever · out of adjust · Nov 10, 2004 · N747DH · Boeing 727224 · Landing Gear Selector
  > DURING TAKEOFF ROLL AT MIO LEFT MAIN GEAR UNSAFE LIGHT FLICKERED OFF AND ON. OPS CHECKED LANDING GEAR CONTROL LEVER POS SWITCH IAW ASTAR MM 32-61-11 PG 401. INDICATIONS NORMAL AT THIS TIME. ALT TEST OK MM 32-61-21 PG 501.
- [SDR DHL2004747006](https://openairdocs.org/sdr/DHL2004747006.md): Line · leaking · Sep 29, 2004 · N747DH · Boeing 727224 · Hydraulic System, Main
  > BEFORE LANDING CVG B HYD SYSTEM QUANTITY WENT TO ZERO QUANTITY HYD SYSTEM B FAILED ABNORMAL PROCEDURE C/W. INSTALLED FLEX LINE BETWEEN B HYD SYSTEM AND FILTER PER GMM CHP 20.1 LEAK CK OK P/N AE 2460010H0360 AND P/N BACH8CO8NN0290.
- [SDR DHL2004747005](https://openairdocs.org/sdr/DHL2004747005.md): Control Unit · inoperative · Aug 4, 2004 · N747DH · Boeing 727224 · Brake Anti-Skid Section
  > MAIN GEAR ANTI- SKID OB INOPERATIVE, (LIGHT REMAINED ILLUMINATED AND IB INOPERATIVE LIGHT WOULD NOT TEST. TO ADD, OB ANTI SKID ILLUMINATED WHILE ON APPROACH. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW MM 32-42-0. NO DEFECTS NOTED.
- [SDR DHL2004747004](https://openairdocs.org/sdr/DHL2004747004.md): Wire · frayed · Mar 16, 2004 · N747DH · Boeing 727224 · Light System Wiring
  > CAPTAIN'S ADJUST LAMP CORD IS FRAYED AND IS ARCING. INSTALLED CLAMP AND TIGHTEN HARDWARE HOLDING GROUND WIRE PER M/M 20-80-1, OPS CHECKED NORMAL PER M/M 33-10-0.
- [SDR DHL2004747003](https://openairdocs.org/sdr/DHL2004747003.md): Door · out of adjust · Feb 11, 2004 · N747DH · Boeing 727224 · Passenger/Crew Doors
  > MAIN ENTRY DOOR DIFFICULT TO CLOSE. ADJUSTED MAIN ENTRY DOOR IAW M/M 52-11-01. OPS CHECKED GOOD.
- [SDR DHL2004747002](https://openairdocs.org/sdr/DHL2004747002.md): Connector · failed · Jan 23, 2004 · N747DH · Boeing 727224 · Engine Pressure Ratio (EPR)
  > NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. (TOGW 144900, IAS 20 KTS, OAT -16 C, 500 FT PA, AND BRAKE ENERGY ZONE NORMAL). TRANSFERRED TO DMI LOG 15488 MEL REF 77-1-1. PLACARDS INSTALLED. REF. DMI 15488 - NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER
- [SDR DHL2004747001](https://openairdocs.org/sdr/DHL2004747001.md): Indicator · inoperative · Jan 16, 2004 · N747DH · Boeing 727224 · Engine Pressure Ratio (EPR)
  > NR 3 EPR INDICATOR INOPERATIVE. WEIGHT: 156000, AIRSPEED: 40 KNOTS, AND OAT -22 C. DEFERRED NR 3 EPR PER MEL 77-1-1 CAT-A DMI 15408.
- [SDR DHL2003747015](https://openairdocs.org/sdr/DHL2003747015.md): Door Frame · cracked · Dec 30, 2003 · N747DH · Boeing 727224 · Fuselage Main, Structure
  > MAIN CARGO DOOR FRAME AFT ACT AREA HAS CRACK. REPAIRED IAW AERONAUTICAL SOLUTIONS REPORT 03-011 IR DTD 12/30/03. MATERIAL USED 2024-T3.090 PO 21582, FASTENERS USED 1103-11 BOLTS, AND HL62-6-9. THIS REPAIR IS A MAJOR REPAIR.
- [SDR DHL2003747014](https://openairdocs.org/sdr/DHL2003747014.md): Door · unsecure · Dec 19, 2003 · N747DH · Boeing 727224 · Emergency Equipment
  > CAPTAIN'S SIDE ESCAPE ROPE DOOR WON'T CLOSE. RE-SECURED DOOR AS REQUIRED; OPS CHECKED NORMAL.
- [SDR DHL2003747012](https://openairdocs.org/sdr/DHL2003747012.md): Power Supply · malfunctioned · Nov 21, 2003 · N747DH · Boeing 727224 · Fuel Flow Indicating
  > IN CRUISE FLIGHT ALL THREE FUEL FLOW GAUGES WENT TO ZERO, S/O ADVISED THAT 28 VDC AND 115 AC FUEL FLOW CIRCUIT BREAKERS HAD POPPED. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY IAW M/M 73-31-12, OPS CHECKED NORMAL IAW JET RUN-UP HANDBOOK 5.2 AND M/M 73-31-0.
- [SDR DHL2003747013](https://openairdocs.org/sdr/DHL2003747013.md): Sleeve · damaged · Nov 4, 2003 · N747DH · Boeing 727224 · Passenger/Crew Doors
  > OUTSIDE MAIN ENTRY DOOR HANDLE WOULD NOT ENGAGE. SPRING ACTION FINE. REMOVED AND REPLACED MAIN ENTRY DOOR HANDLE MECHANICAL SLEEVE PER B-727 M/M 52-11-01. OPS CHECKED GOOD PER B-727 M/M 52-11-01 PAGE 501.
- [SDR DHL2003747011](https://openairdocs.org/sdr/DHL2003747011.md): Light · inoperative · Oct 11, 2003 · N747DH · Boeing 727224 · Emergency Lighting
  > ENTRY EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00. OPS CHECKED GOOD.
- [SDR DHL2003747010](https://openairdocs.org/sdr/DHL2003747010.md): Light · malfunctioned · Aug 27, 2003 · N747DH · Boeing 727224 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR ILLUMINATED. EMERGENCY EXIT LIGHT NOT ILLUMINATED PER 33-50-01 PAGE 7. THE 2-28V BULBS ILLUMINATED WITH NO SMOKING SWITCH IN ON POSITION. TURNED SWITCH OFF LIGHTS EXTINGUISHED.
- [SDR DHL2003747009](https://openairdocs.org/sdr/DHL2003747009.md): Snubber · out of adjust · Jul 30, 2003 · N747DH · Boeing 727224 · Passenger/Crew Doors
  > ON TOUCHDOWN FORWARD ENTRY DOOR HANDLE POPPED OPEN. ADJUSTED ENTRY DOOR SNUBBERS, OPS CHECKED GOOD IAW 52-11-0.
- [SDR DHL2003747008](https://openairdocs.org/sdr/DHL2003747008.md): Downlock Sensor · faulty · Jun 26, 2003 · N747DH · Boeing 727224 · Landing Gear Position and Warning
  > WHEN LANDING GEAR LOWERED, RIGHT GEAR RED LIGHT ILLUMINATED WITH RIGHT GEAR GREEN LIGHT OUT. SECONDARY MAIN GEAR POSITION INDICATOR GREEN LIGHTS BOTH ON. COMPLETED ABNORMAL PROCEDURES PER AOM 6.2.69. REPLACED RIGHT GEAR DOWN LOCK SENSOR. OPS NORMAL IAW MM
- [SDR DHL2003747006](https://openairdocs.org/sdr/DHL2003747006.md): Engine · malfunctioned · Jun 10, 2003 · N747DH · Boeing 727224 · Turbine Engine Oil System
  > IN-FLIGHT ENGINE NR 1 OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURES, SHUT DOWN ENGINE AS PER ABNORMAL PROCEDURES. DIVERTED TO KMCI. ON SHORT FINAL, LIGHT DID EXTINGUISH. INSPECTED FILTER, CHECKED GOOD. LEAK CHECKED GOOD ON ENGINE RUN.
- [SDR DHL2003747509](https://openairdocs.org/sdr/DHL2003747509.md): Support · cracked · May 14, 2003 · N747DH · Boeing 727224 · Leading Edge Devices
  > DURING C CHECK, UPON REMOVAL OF NR 7 SLAT ACTUATOR SUPPORT STRUCTURE FOUND O/B MOUNT CRACKED AND I/B MOUNT CHAFED. REMOVED FUEL TANK ACCESS PANEL 7615 AND 7618 IAW B-727 M.M. 28-11-21. REMOVED DAMAGED ANGLES AND INSTALLED NEW FABBED FROM BAC1503-100145 P.O.
- [SDR DHL2003747517](https://openairdocs.org/sdr/DHL2003747517.md): Intake Duct · cracked · May 13, 2003 · N747DH · Boeing 727224 · Engine Air Intake System
  > DURING C-CHECK, N/R 53639 EMP STA 1303 WEB ABOVE NR 2 ENGINE INTAKE DUCT IS CRACKED, LOWER RT CORNER. REMOVED FASTENERS FOR ACCESS PER B-727 SRM 51-30-2. STOP DRILL AT WEB STA 1303 PER SERVICE BULLETIN 727-53-0094, REV 3 HFEC PER 727 NDT PT6-51-00-00 FIG 23.
- [SDR DHL2003747516](https://openairdocs.org/sdr/DHL2003747516.md): Stringer · corroded · May 13, 2003 · N747DH · Boeing 727224 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, N/R 53605 IN AFT CARGO STR 27L HAS CORROSION FROM BS 950 A TO BS 1070. CUT-OUT DAMAGED SECTION OF STR 27 L FROM STA 950A PLUS 10 TO 1080 IAW B-727 SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER USING BAC1498-145 4 PIECES AT 21 INCHES, TWO EACH AT
- [SDR DHL2003747515](https://openairdocs.org/sdr/DHL2003747515.md): Skin · dented · May 13, 2003 · N747DH · Boeing 727224 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, N/R 53604 IN AFT CARGO FRAME BS 1050 HAS A DENT INTO THE RADIUS BELOW STR 26 L. CUT OUT DAMAGED AREA DIM 1 INCH X 1 INCH AND FABRICATED ONE DOUBLER DIMENSIONS 10 INCH X 6 INCH USING 7075-T6.071 PO 9912380 IAW B-727 SRM 51-40-3 FIG 1. ALODINE
- [SDR DHL2003747512](https://openairdocs.org/sdr/DHL2003747512.md): Skin · dented · May 13, 2003 · N747DH · Boeing 727224 · Fuselage Main, Plate/Skin
  > DURING "C" CHECK, N/R 53655, CABIN INTERIOR AT BS 560 DENT AND CRACK BTW. ST. 16R-17R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREAS DIMENSIONS 1 X 1 INCH IAW B-727 SRM 51-40-3 FIG. 1. FABRICATED ANGLE REPAIR USING 7075-T6.063
- [SDR DHL2003747510](https://openairdocs.org/sdr/DHL2003747510.md): Stiffener · cracked · May 13, 2003 · N747DH · Boeing 727224 · Leading Edge Devices
  > DURING "C" CHECK N/R 53650 LT WING LE CAVITY LE STA. 1307 VERTICAL STIFFENER IS CRACKED AT BOTTOM END (FRONT SPAR WBL 92.8. REMOVED L/H WING ACCESS PANEL 6303 TO FACILITATE SM WORK IAW B-727 M.M. 57-30-0. REMOVED LT WING FUEL TANK ACCESS 7340 TO FACILITATE S
- [SDR DHL2003747506](https://openairdocs.org/sdr/DHL2003747506.md): Frame · dented · May 13, 2003 · N747DH · Boeing 727224 · Fuselage Main, Frame
  > DURING "C" CHECK IN AFT. CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS BELOW STR 26L. CUT-OUT DAMAGE AREA APROX 1 INCH FRAME 1030 STR 26 L IAW B-727 S.R.M. 51-40-3. 2) REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. 3)

Next page: https://openairdocs.org/deregistered/N747DH-2017-10-31/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N747DH' AND deregistration_id = 'N747DH-2017-10-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N747DH-2017-10-31/reports

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